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2 February 2026

A Note on Chaos of a Modified Piecewise Linear Discontinuous System with Multiple-Well Potentials: Melnikov Approach with Simulations

,
and
1
Institute of Mathematics and Informatics, Bulgarian Academy of Sciences, Acad. G. Bonchev Str., Bl. 8, 1113 Sofia, Bulgaria
2
Centre of Excellence in Informatics and Information and Communication Technologies, 1113 Sofia, Bulgaria
3
Faculty of Mathematics and Informatics, Sofia University “St. Kliment Ohridski”, 5, James Bourchier Blvd., 1164 Sofia, Bulgaria
4
Faculty of Mathematics and Informatics, University of Plovdiv Paisii Hilendarski, 24, Tzar Asen Str., 4000 Plovdiv, Bulgaria
This article belongs to the Special Issue Complex Networks and Dynamical Systems

Abstract

The topic of chaotic thresholds for piecewise linear discontinuous (PWLD) systems with multiple-well potentials is a persistent topic in the research of a number of authors. In this article we investigate the chaos of a modified piecewise linear discontinuous (MPWLD) system. The model, containing N free parameters, could be of interest to specialists working in this area. With a specially developed software product, we generate the Melnikov equation M ( t ) = 0 and examine all its zeros. This opens up an opportunity for researchers to correctly understand and formulate the classical Melnikov criterion for the possible occurrence of chaos in dynamical systems. Several simulations are composed. We also demonstrate some specialized modules for investigating the dynamics of the proposed model. Intriguing and new generalizations made through probabilistic constructions are considered.

1. Introduction

Studies on the equilibrium bifurcation problem of non-smooth systems were first reported in 1949 by Andronov [1].
It is well known that piecewise linear systems are typical non-smooth dynamics systems that often occur in engineering and science [2,3,4,5,6].
Various types of discontinuous dynamical systems [7] have been studied in the literature, including the Filippov-type discontinuity; the discontinuous right-hand side [8]; dry friction dampers [9,10]; phase-state discontinuities, such as impacting systems [11,12]; and also systems with a non-smooth Jacobian matrix [13,14].
Many authors devote their research to this interesting topic.
The detection of grazing orbits and incident bifurcations of a forced continuous piecewise linear oscillator is considered by Hu [15].
Bernardo and Hogan [16] present an overview of the discontinuity-induced bifurcations of piecewise smooth dynamical systems.
Canards in piecewise linear system explosions and super-explosions can be found in [17].
Archetypal oscillators for smooth and discontinuous dynamics are discussed in [18,19].
Chaotic oscillations in a piecewise linear spring–mass system are considered in [20].
For a bifurcation analysis of a smooth-and-discontinuous oscillator, see [21,22,23].
The chaotic behavior of oscillators with strong irrational nonlinearities and second-order piecewise linear systems is considered in [24,25,26].
The reader can find interesting considerations about Melnikov functions for singularly perturbed ordinary differential equations in [27].
These studies range from theoretical formulations and methodologies to applications in engineering science.
Ref. [28] shows that some knowledge of differential equations can be generalized for discontinuous systems.
The most attention has been focused on planar systems with a homoclinic trajectory that have been perturbed by a periodic function. It was proved, under additional assumptions, that this perturbed system has a homoclinic solution again.
The proof is based on the existence of simple zeroes of a “non-smooth” Melnikov function.
It was shown [28] that if we want to use the Melnikov method, we need the existence and continuity of the second derivative of the right-hand side out of the discontinuity surface.
More precisely, Kukuchka [28] also notes the following: “…For example, we could consider other perturbations instead of periodic ones or we could deal with the Melnikov method for systems in R n , n 2 , but the most interesting case would be to remove the restriction of transversal intersections through the discontinuity surface. This should be an initiative for the next study.”.
Detailed information on other difficulties that researchers encounter in the direct application of Melnikov’s theory can be found in the monographic study in [29].
For other results, see [30,31].
Many studies on friction oscillator models, semi-dynamical systems, and other mechanisms are based on Filippov regularization. For more details, see [32,33,34,35,36,37].
In [38], the authors consider the following piecewise linear discontinuous system with multiple-well potentials:
d x d t = y , d y d t = 2 x + sign ( x + α ) + sign ( x α ) ϵ a y f cos ( ω t ) .
With the help of the Hamiltonian function ( ϵ = 0 ), the authors study all special homo–heteroclinic-like orbits [38]:
( x ± 1 ( t 1 ) , y ± 1 ( t 1 ) ) = ( ± 1 ± cos 2 t 1 , 2 sin 2 t 1 ) ( 0 , 0 )
for t 1 π 2 , π 2 ;
( x ± 2 ( t 1 ) , y ± 2 ( t 1 ) ) = ( ± 1 ± ( 1 α ) cos 2 t 1 , ( 1 α ) 2 sin 2 t 1 ) ( ± α , 0 )
for t 1 π 2 , π 2 ;
( x ± 3 ( t 2 ) , y ± 3 ( t 2 ) ) = ( ± α sin 2 t 2 , ± α 2 cos 2 t 2 ) ( ± α , 0 )
for t 2 π 2 2 , π 2 2 ;
( x ± 4 ( t 2 ) , y ± 4 ( t 2 ) ) = ( ± sin 2 t 2 , ± 2 cos 2 t 2 ) ( ± 1 , 0 )
for t 2 π 2 2 , π 2 2 .
The Melnikov criterion for generating chaos in system (1) is also discussed.
In this paper we consider a generalization of differential system (1).
We study chaos in the proposed new model.
Several simulations are composed. We also demonstrate some specialized modules for investigating the dynamics of the model.
Intriguing generalizations made through probabilistic constructions are considered.

2. A New Generalized Model: Melnikov Approach

We consider the new modified dynamical system of the form:
d x d t = y , d y d t = 2 x + sign ( x + α ) + sign ( x α ) ϵ A y j = 1 N g j cos ( j ω t ) ,
where 0 ϵ < 1 , A is the damping level, g i 0 ; i = 1 , , N , and N is integer.
The Melnikov function [39] gives a measure of the leading-order distance between the stable and unstable manifolds when ϵ 0 and can be used to tell where the stable and unstable manifolds intersect transversely.
By definition, the Melnikov integral is given by
M ± i ( t 0 ) = A y ± i ( t ) 2 + y ± i ( t ) j = 1 N g j cos ( j ω ( t + t 0 ) ) d t , i = 1 , 2 , 3 , 4 .
From a numerical point of view, the task of finding all roots of M ± i ( t 0 ) , i = 1 , 2 , 3 , 4 is interesting, given that the parameters appearing in the proposed differential model are subject to a number of restrictions of a physical and practical nature.
We can prove the following proposition when N = 2 .
Proposition 1.
If N = 2 , then the roots of the Melnikov function M ± i ( t 0 ) , i = 1 , 2 , 3 , 4 , are given as solutions of the following equations:
M + 1 ( t 0 ) = 2 A π + 4 g 1 sin ( π ω 2 ) 2 + ω 2 sin ( t 0 ω ) + 2 g 2 sin ( 2 π ω ) 1 + 2 ω 2 sin ( 2 t 0 ω ) = 0 ; M + 2 ( t 0 ) = 2 A π ( 1 + α ) 2 + ( 1 + α ) 4 g 1 sin ( π ω 2 ) 2 + ω 2 sin ( t 0 ω ) + 2 g 2 sin ( 2 π ω ) 1 + 2 ω 2 sin ( 2 t 0 ω ) = 0 ; M 3 ( t 0 ) = A π α 2 2 + 4 g 1 α cos ( π ω 2 2 ) 2 + ω 2 cos ( t 0 ω ) + 2 g 2 α cos ( π ω 2 ) 1 + 2 ω 2 cos ( 2 t 0 ω ) = 0 ; M 4 ( t 0 ) = A π 2 + 4 g 1 cos ( π ω 2 2 ) 2 + ω 2 cos ( t 0 ω ) + 2 g 2 cos ( π ω 2 ) 1 + 2 ω 2 cos ( 2 t 0 ω ) = 0 .
For example, the Melnikov function M 4 ( t 0 ) for N = 2 in case (A), A = 0.009 , ω = 0.879 , g 1 = 0.09 , g 2 = 0.16 , is depicted in Figure 1. (In this case, the Melnikov function is a trigonometric polynomial that has two simple zeros in the considered interval).
Figure 1. Equation M 4 ( t 0 ) = 0 (Proposition 1); case (A).
Case (B): A = 0.006 , ω = 0.08 , g 1 = 0.39 , g 2 = 0.26 . In this case, the Melnikov polynomial has root t 0 = 3.11969 with multiplicity two (see Figure 2).
Figure 2. Equation M 4 ( t 0 ) = 0 (Proposition 1); case (B).
We can prove the following proposition when N = 3 .
Proposition 2.
If N = 3 , then the roots of the Melnikov function M 3 ( t 0 ) are given as solutions of the following equation:
M 3 ( t 0 ) = A π α 2 2 + 4 α g 1 cos ( π ω 2 2 ) 2 + ω 2 cos ( t 0 ω ) + 2 g 2 α cos ( π ω 2 ) 1 + 2 ω 2 cos ( 2 t 0 ω ) + 4 g 3 α cos ( 3 π ω 2 2 ) 2 + 9 ω 2 cos ( 3 t 0 ω ) = 0 .
For example, the Melnikov function M 3 ( t 0 ) for N = 3 , α = 0.5 in case (A), A = 0.009 , ω = 0.879 , g 1 = 0.09 , g 2 = 0.16 , g 3 = 0.3 , is depicted in Figure 3. (In this case the Melnikov polynomial has three simple zeros.)
Figure 3. Equation M 3 ( t 0 ) = 0 (Proposition 2); case (A).
Case (B): A = 0.005 , ω = 0.9 , g 1 = 0.135 , g 2 = 0.21 , g 3 = 0.3 . In this case the Melnikov polynomial has one simple zero and root t 0 2.52 with multiplicity two (see Figure 4).
Figure 4. Equation M 3 ( t 0 ) = 0 (Proposition 2); case (B).
Melnikov criterion. If M ( t 0 ) = 0 and d M ( t 0 ) d t 0 0 for some t 0 and some sets of parameters, then this indicates the possibility of chaotic dynamics under the stated assumptions.
From Propositions 1 and 2, the reader may formulate the Melnikov criterion for the intersection of projections of separatrixes onto the phase plane and possibly chaos.

3. Some Simulations

We will look at some interesting simulations using model (2):
Example 1.
For N = 4 , α = 0.95 , A = 0.01 , ω = 0.01 , g 1 = 0.6 , g 2 = 0.2 , g 3 = 0.3 , g 4 = 0.8 , ϵ = 0.1 , the simulations on system (2) for x 0 = 0.2 , y 0 = 0.1 are depicted in Figure 5.
Figure 5. (a) x-component of the solutions of system (2); (b) y-component of the solutions of system (2); (c) phase space (Example 1).
Example 2.
For N = 6 , α = 0.15 , A = 0.01 , ω = 0.01 , g 1 = 0.6 , g 2 = 0.2 , g 3 = 0.3 , g 4 = 0.8 , g 5 = 0.1 , g 6 = 0.7 , ϵ = 0.1 , the simulations on system (2) for x 0 = 0.1 , y 0 = 0.1 are depicted in Figure 6.
Figure 6. (a) x-component of the solutions of system (2); (b) y-component of the solutions of system (2); (c) phase space (Example 2).
Example 3.
For N = 7 , α = 0.01 , A = 0.07 , ω = 0.01 , g 1 = 0.01 , g 2 = 0.12 , g 3 = 0.2 , g 4 = 0.4 , g 5 = 0.1 , g 6 = 0.1 , g 7 = 0.5 , ϵ = 0.02 , the simulations on system (2) for x 0 = 0.1 , y 0 = 0.1 are depicted in Figure 7.
Figure 7. (a) x-component of the solutions of system (2); (b) y-component of the solutions of system (2); (c) phase space (Example 3).
Example 4.
For N = 9 , α = 0.95 , A = 0.07 , ω = 0.01 , g 1 = 0.06 , g 2 = 0.12 , g 3 = 0.3 , g 4 = 0.18 , g 5 = 0.1 , g 6 = 0.2 , g 7 = 0.3 , g 8 = 0.05 , g 9 = 0.4 , ϵ = 0.18 , the simulations on system (2) for x 0 = 0.4 , y 0 = 0.3 are depicted in Figure 8.
Figure 8. (a) x-component of the solutions of system (2); (b) y-component of the solutions of system (2); (c) phase space (Example 4).
Example 5.
For N = 11 , α = 0.97 , A = 0.1 , ω = 0.01 , g 1 = 0.3 , g 2 = 0.15 , g 3 = 0.05 , g 4 = 0.25 , g 5 = 0.15 , g 6 = 0.25 , g 7 = 0.1 , g 8 = 0.1 , g 9 = 0.9 , g 10 = 0.95 , g 11 = 1.05 , ϵ = 0.107 , the simulations on system (2) for x 0 = 0.45 , y 0 = 0.3 are depicted in Figure 9.
Figure 9. (a) x-component of the solutions of system (2); (b) y-component of the solutions of system (2); (c) phase space (Example 5).
The reader can also consider other interesting examples that demonstrate the variety of phase portraits depending on the variation of the parameter α in the considered interval [ 0 , 1 ] , and for this reason we will not dwell on these demonstrations here.

4. Further Generalizations Through Probabilistic Constructions

Let us slightly modify model (2) by changing the sign function with the indicator function 2 I x 0 1 :
d x d t = y , d y d t = 2 I x α + I x α x 1 ϵ A y j = 1 N g j cos j ω t .
We shall now generalize model (6) in two directions. First, let the function G · stand for the step part:
G x = I x α + I x α .
Its behavior (for α = 1 ) can be seen in Figure 10a. One can recognize the double cumulative distribution function (CDF) of a distribution with atoms in the points α and α with probabilities 1 2 . Hence, we can generalize the dynamics (6) by using an arbitrary distribution with CDF F · , as well as different weights for the non-perturbed terms:
d x d t = y , d y d t = b 1 F x b 2 x b 3 ϵ A y j = 1 N g j cos j ω t .
The importance of generalization (8) is in several directions. On one hand, introduction of the coefficients b 1 , b 2 , and b 3 is a more or less technical assumption but it gives the user more flexibility. Note that the term x 1 in (6) is a downward compensator whose force can be controlled through b 1 , b 2 , and b 3 in (8). On the other hand, the most important factor is the CDF that replaces the indicator part (7). In the original model (6), the indicators play the role of a jump impulse from one state to another for the derivative of the y-component with respect to the position of the x-term (with respect to ± α ). Thus, by introducing a CDF which combines a continuous part with atoms, we can incorporate a suitable continuous dependence of the y-derivative between the jumps that occur in the atoms. Also, the probability at an atom gives the jump size for the y-derivative at this place.
Figure 10. Oscillators based on the Exponential distribution.
We can generalize further using the complex presentation of the cos function:
cos x = e i x + e i x 2 .
Let K = k = 1 N g k and g ¯ j = g j K . Let ξ be a random variable distributed on the set 1 , 2 , , N with probabilities g ¯ k . Let its characteristic function be denoted by ψ x . We can rewrite the y-dynamics of (6) as
d y d t = b 1 F x b 2 x b 3 ϵ K A y k = 1 N g ¯ k cos k ω t = b 1 F x b 2 x b 3 ϵ K A y k = 1 N g ¯ k e i k ω t + e i k ω t 2 = b 1 F x b 2 x b 3 ϵ K A y E e i ω t ξ + E e i ω t ξ 2 = b 1 F x b 2 x b 3 ϵ K A y 1 2 ψ ω t + ψ ω t ,
where E stands for the mathematical expectation. We can use an arbitrary random variable distributed on a domain D instead of the set 1 , 2 , , N . This way, the sum in dynamics (6) should be changed into an integral:
d y d t = b 1 F x b 2 x b 3 ϵ K A y D cos u ω t g d u ,
where g · is the density function. Thus, we transform the original dynamics (2) into
d x d t = y , d y d t = b 1 F x b 2 x b 3 ϵ K A y 1 2 ψ ω t + ψ ω t .
Having in mind this presentation, we rewrite Melnikov integral (3) as
M ± i t 0 = A y ± i t 2 + y ± i t 2 ψ ω t + t 0 + ψ ω t + t 0 d t , i = 1 , 2 , 3 , 4 .
Let us discuss an example for which the random variable that drives the perturbations is exponentially distributed and thus its characteristic function is
ψ x = β β i x .
Hence,
ψ x + ψ x = 2 β 2 β 2 + x 2 .
Thus, dynamics (12) turns into
d x d t = y , d y d t = b 1 F x b 2 x b 3 ϵ K A y β 2 β 2 + ω 2 t 2 ,
whereas Melnikov integral (13) is
M ± i t 0 = A y ± i t 2 + y ± i t β 2 β 2 + ω 2 t + t 0 2 d t , i = 1 , 2 , 3 , 4 .
Unfortunately, Melnikov integral (17) cannot be evaluated through closed-form formulas and thus some numerical methods have to be applied.
We continue with our example considering the following CDF F · that combines a Gaussian function and atoms:
F x = c 1 N x , x < α 1 c 2 N x , x α 1 , α 2 N x , x α 2 ,
where 0 < c 1 < c 2 < 1 and N x is the CDF of the standard normal distribution:
N x = 1 2 π x e u 2 2 d u .
Function (18) is depicted in Figure 10b for the following values of the parameters: α 1 = 0.1 , α 2 = 0.5 , c 1 = 0.3 , and c 2 = 0.6 .
The behavior of this oscillator is presented in Figure 10c (x-dynamics), Figure 10d (y-dynamics), and Figure 10e (phase portrait). In addition to the above-applied parameters, we use b 1 = 5 , b 2 = 2 , b 3 = 1.5 , ϵ = 0.1 , K = 1 , A = 0.2 , ω = 1.01 , β = 0.3 , x 0 = 0.6 , and y 0 = 0.7 .
Last but not least, we shall discuss the perturbation term in dynamics (12). We can observe that the periodicity vanishes for the exponential distribution—see system (16). It turns out that this is due to some convergence reasons. To confirm this, we shall consider the exponential distribution as a limit of a sequence of suitable geometric distributions. For every n > β , let ξ n be a geometrically distributed random variable with the success rate p n = β n and let the random variable η n be defined as η n = ξ n n . We can observe for the cumulative distribution function when n tends to infinity:
lim n P η n < x = lim n P ξ n < n x = lim n 1 1 β n n x = 1 e β x .
Above, we denote by x the integer part of x. One can recognize the cumulative distribution function of the exponential distribution in the last term of (20). Let us consider a geometric distribution with success rate p for the perturbation term of dynamics (12). We can easily derive
ψ x + ψ x 2 = p 2 e i x 1 1 p e i x + e i x 1 1 p e i x = p cos x 1 + p 1 + 1 p 2 2 1 p cos x .
Thus, model (12) turns into
d x d t = y , d y d t = b 1 F x b 2 x b 3 ϵ K A y p cos ω t 1 + p 1 + 1 p 2 2 1 p cos ω t .
We can conclude that the periodicity in the perturbation terms still exists. We need to slightly modify dynamics (22) since the geometrically distributed random variable is not η but ξ n = n η . Hence, the following relation between the characteristic functions stands:
ψ η x ψ n x = ψ ξ n x n .
Having in mind that
lim n n 1 cos x n 0 , lim n 2 n 2 1 cos x n x 2 ,
we obtain
lim n ψ n x + ψ n x 2 = lim n β n cos x n 1 + β n 1 + 1 β n 2 2 1 β n cos x n = lim n β n cos x n 1 + β 2 n 2 + n β 2 2 n n β cos x n = lim n β n cos x n 1 + β 2 2 n 2 1 cos x n 2 β n 1 cos x n + β 2 = β 2 β 2 + x 2 .
Of course, this is the term for the exponential distribution—see formula (15)—and it leads to dynamics (16). Thus, we confirm that the vanishing periodicity is due to convergence reasons and this does not terminate the validity of our model.
Finally, let us give another example with a continuous distribution that keeps the periodicity. If we consider the normal distribution with mean μ and variance σ 2 , then
ψ x = e i μ x σ 2 x 2 2 .
Hence,
ψ x + ψ x 2 = e σ 2 x 2 2 e i μ x + e i μ x 2 = e σ 2 x 2 2 cos μ x .
Thus, model (12) turns into
d x d t = y , d y d t = b 1 F x b 2 x b 3 ϵ K A y e σ 2 ω 2 t 2 2 cos μ ω t .
We can observe a time decay in addition to the periodicity in the perturbations. Melnikov integral (13) turns into
M ± i t 0 = A y ± i t 2 + y ± i t e σ 2 ω 2 t + t 0 2 2 cos μ ω t + t 0 d t . i = 1 , 2 , 3 , 4 .
One can evaluate the integrals above via an imaginary error function. We omit this since it is technical and does not provide significant facilities beyond the numerical approximation of the integrals.
To confirm this convergence, we jointly plot the phase portraits for different values of n in Figure 10f—they are n = 1 , n = 3 , and n = 20 . As we mentioned above, we have modified dynamics (22) through relation (23) to reach
d x d t = y , d y d t = b 1 F x b 2 x b 3 ϵ K A y p cos ω t n 1 + p 1 + 1 p 2 2 1 p cos ω t n .
We can see that the phase portraits differ but have one and the same shape. Furthermore, the model for n = 20 practically coincides with the exponential model.

5. Concluding Remarks

The main research directions in this article are as follows:
(a) The possibility of using correcting perturbation factors containing many free parameters for modifying classical and newer dynamic models;
(b) Further generalizations through probabilistic constructions; see Section 4. An explicit representation of the Melnikov integral through the corresponding characteristic function is also proposed.
Given the issues raised in this work, we look forward to more research on this intriguing subject. The computation of Lyapunov exponents, the construction of bifurcation diagrams, the use of Poincaré maps, clearing parameter ranges in the two-dimensional model, and summarizing sufficient or necessary conditions for the occurrence of chaos will all be covered in this analysis. Additionally, a more systematic discussion of the Melnikov criterion’s applicability conditions in the presence of multi-frequency perturbations will be provided, along with a systematic discussion of how the dynamical complexity changes as the parameter N increases, as well as long-term trajectory simulations.
The reader can consider the corresponding approximation problem for an arbitrarily chosen N.
Example 6.
To generate the Melnikov polynomial M 3 ( t 0 ) for fixed N = 5 and the constraints | I m ( ω ) | < 1 5 .
The solution to the given problem using our specialized module is visualized in Figure 11.
Figure 11. The Melnikov polynomial M 3 ( t 0 ) generated using our specialized module (Example 6).
Some two-sided methods for simultaneous determination of all roots of trigonometric and exponential polynomials of the type M ( t 0 ) = 0 are considered in [40].
The derived results can be used as an integral part of a much more general application for scientific computing—for some details, see [41].
We will explicitly note that some perturbed correction factors used in [42,43,44,45,46,47] can be used successfully to track the dynamics of modified models of type (2).
The reader can also consider other examples of chaotic seas and co-existing periodic orbits found when varying the external frequency ω for fixed values of the free parameters g i (N in number) based on the modified piecewise differential model proposed in this article.
Of course, the determination of the existence of chaos of this hypothetical model is up to the specialists working in this scientific field.
We will share with the readers some aspects related to our vision for teaching elements of this interesting dynamic theory to our students, see Appendix A. Of course, the topic is open for future discussions.
In our future work, we envisage studying the dynamics of modified models, known in the engineering literature as oscillators with “stops” (see, for example, [48,49]), including the study of the limiting discontinuous case, in light of the results obtained in this paper.

Author Contributions

Conceptualization, T.Z., N.K. and A.I.; methodology, T.Z. and N.K.; software, T.Z. and A.I.; validation, N.K. and T.Z.; formal analysis, N.K., A.I. and T.Z.; investigation, T.Z., A.I. and N.K.; resources, N.K., A.I. and T.Z.; data curation, A.I. and T.Z.; writing—original draft preparation, T.Z., N.K. and A.I.; writing—review and editing, A.I., T.Z. and N.K.; visualization, T.Z. and A.I.; supervision, A.I. and T.Z.; project administration, T.Z. and N.K.; funding acquisition, N.K., A.I. and T.Z. All authors have read and agreed to the published version of the manuscript.

Funding

The work was supported by the Centre of Excellence in Informatics and ICT under the Grant No BG16RFPR002-1.014-0018-C01, financed by the Research, Innovation and Digitalization for Smart Transformation Programme 2021-2027 and co-financed by the European Union.

Data Availability Statement

The original contributions presented in this study are included in the article. Further inquiries can be directed to the corresponding author.

Conflicts of Interest

The authors declare no conflicts of interest.

Appendix A. Challenges for Learners

We offer an efficient learning strategy that emphasizes learning and challenges our master’s and doctoral students to consider the triangle of enigmatics, creativity, and acmeology.
After providing curriculum modules we will set the following tasks for self-learning.
Probably, the correction factor j = 1 n g j cos ( j ω t ) used in our model (2) can be used to obtain the new modified dynamical system of the form:
d x d t = y , d y d t = 3 x + sign ( x + α ) + sign ( x ) + sign ( x α ) ϵ A y j = 1 N g j cos ( j ω t ) ,
where 0 ϵ < 1 , A is the damping level, g i 0 ; i = 1 , , N , and N is integer.
Task 1 (self-learning).
(a) Study the chaotic behavior of this new model with the methodology proposed in this article.
(b) Let N = 4 , α = 0.35 , A = 0.01 , ω = 0.2 , ϵ = 0.09 . For what values of the parameters g i , i = 1 , 2 , 3 , 4 is the dynamics depicted in Figure A1 obtained?
Figure A1. (a) x-component of the solutions of the new modified dynamical system; (b) y-component of the solutions of the new modified dynamical system; (c) phase space (Task 1 (self-learning)).
Figure A1. (a) x-component of the solutions of the new modified dynamical system; (b) y-component of the solutions of the new modified dynamical system; (c) phase space (Task 1 (self-learning)).
Axioms 15 00109 g0a1
(c) Draw the corresponding conclusions.
(Answer: when performing the task correctly, you should get the following approximate values: g 1 = 2.6 , g 2 = 1.2 , g 3 = 2.3 , g 4 = 1.8 )
(d) Propose new generalizations through probabilistic constructions based on the considerations in Section 4.
Task 2 (self-learning). Study the behavior of the new model at fixed values: N = 9 ; α = 0.3 ; A = 0.008 ; ω = 0.23 ; g 1 = 1.6 , g 2 = 0.2 , g 3 = 1.3 , g 4 = 0.8 , g 5 = 1.1 , g 6 = 1.2 , g 7 = g 8 = 0 , g 9 = 2 .
(a) For what value of the parameter ϵ ( 0 < ϵ 1 ) is the phase portrait depicted in Figure A2 obtained?
Figure A2. (Phase portrait (Task 2 (self-learning))).
Figure A2. (Phase portrait (Task 2 (self-learning))).
Axioms 15 00109 g0a2
(Answer: when performing the task correctly, you should get the following approximate value: ϵ = 0.015 )
(b) Show a chaotic phase portrait/sensitive dependence for parameters above this threshold.
(c) Draw the corresponding conclusions.
Our conclusion as teachers is that with the proposed methodology, students adapt relatively well and touch upon the Andronov–Melnikov theory for the possible occurrence of chaos in the dynamical system under consideration.

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